适用于探空火箭的图像采集与压缩系统

针对探空火箭遥测带宽低、图像监控通路多、系统小型化等设计难点,提出一种基于ADV212的图像采集与压缩系统设计方案。采用可以同时支持无损和高压缩比有损压缩的JPEG2000图像压缩标准,提出适用于箭上图像采集特点的通道切换和中断处理策略,并以"乒乓"操作的流水线作业方式实现多路图像通道数据吞吐,通过两个实时发送通道和一个缓存发送通道向火箭遥测链路发送图像数据。提出一种具有动态帧频和压缩比的图像压缩方案,解决了探空火箭遥测带宽有限这一问题。本设计以Virtex-4系列现场可编程门阵列作为系统控制核心,采用ADV7182和ADV212分别完成图像的采集和压缩,分别采用静态随机存取存储器和同步动态随机存储器实现图像的实时传输和缓存传输。通过比较图像间的峰值信噪比值,试验并分析了适用于电荷耦合元件图像的压缩滤波器和小波变换级数,得到了较为满意的图像质量。设计较好地满足了本次空间环境垂直探测探空火箭的图像采集任务。     

最优停止理论中离散化方法的应用

离散化方法是研究连续参数最优停止理论和马尔可夫过程最优停止理论的有效方法。本文对这一方法进行了阐述，并用此方法解决了两个实际问题。     

简支扁壳弯曲问题的一般解

本文建立了四边简支的矩形扁壳弹性弯曲问题的一般解析解。以面内四边位移为零的简支矩形扁壳为例求解了匀布荷载作用下的对称变形解。     

采用多模式控制的电磁发射蓄电池充电谐波抑制方法

针对电磁发射蓄电池组大倍率快速充电过程中的电网谐波陡增问题,提出多模式模糊滞环控制谐波抑制方法。结合电磁发射混合储能系统的时序串联拓扑结构,说明蓄电池的超大倍率充电应用工况和策略,进而介绍蓄电池充电的拓扑结构,明确谐波的来源、特点和产生原因。在分析单台充电机充电时的电网谐波电压和谐波电流的基础上,研究不同充电机并充台数、不同充电电流情况下电网谐波电压和谐波电流的分布规律。设计多模式控制方法的组成方式和切换判据,建立蓄电池充电机、瞬时无功功率检测、谐波抑制、多模式控制的仿真模型。仿真和试验数据表明：谐波抑制方法能够快速抑制电磁发射蓄电池充电机大规模启停、波动时的谐波陡增问题,补偿效果满足国家标准。     

某型飞机魔球信号采集与分析

从阐述魔球操作对目标瞄准的实现机制入手,分析了数据采集系统的总体结构及采集系统的硬件设计和软件设计思想.实现了对飞机魔球信号的实时采集,并对采集结果进行仿真分析,从而推导出不同相关武器种类、目标与弹轴不同夹角、不同目标距离、不同工作状态下魔球信号的变化规律.     

Hypersonic impact flash characteristics of a long-rod projectile collision with a thin plate target

Impact flash occurs when objects collide at supersonic speeds and can be used for real-time damage assessment when weapons rely on kinetic energy to destroy targets.However,the mechanism of impact flash remains unclear.A series of impact flash experiments of flat-head long-rod projectiles impacting thin target plates were performed with a two-stage light gas gun.The impact flash spectra for 6061 aluminum at 1.3-3.2 km/s collision speeds were recorded with a high-speed camera,a photoelectric sensor,and a time-resolved spectrometer.The intensity of the impact flash exhibited a pulse charac-teristic with time.The intensity(I)increased with impact velocity(V0)according to I∝Vn0,where n = 4.41 for V0 ＞ 2 km/s.However,for V0 ＜ 2 km/s,n = 2.21,and the intense flash duration is an order of magnitude less than that of higher V0.When V0 ＞ 2 km/s,a continuous spectrum(thermal radiation background)was observed and increased in intensity with V0.However,for V0 ＜ 2 km/s,only atomic line spectra were detected.There was no aluminum spectral lines for V0 ＜ 2 km/s,which indicated that it had not been vaporized.The initial intense flash was emission from excited and ionized ambient gases near the impact surface,and had little relationship with shock temperature rise,indicating a new mechanism of impact flash.     

装甲装备动用制度改革浅析

装甲装备动用制度是装备管理工作的核心,动用制度的好坏直接关系到装备的战备完好率、寿命周期费用,以及战斗力的形成.通过对现行装备动用制度进行研究分析,提出了装甲装备动用制度改革的基本思路,并进行了可行性论证.     

The mechanism of liquid dispersing from a cylinder driven by central dynamic shock loading

A systematic investigation on the mechanism of dynamic liquid dispersing process via theoretical and experimental approach is presented. The experiments include weak and strong constrained scenarios using the high-speed camera technique and the flash X-ray radiography technique. Based on dynamic analysis, one-dimensional characteristics analysis and some numerical simulations on the propagating processes of blast waves before the container shell rupturing, further and detailed analyses of the experimental results are presented. The effects of the liquid viscosity on the dynamic dispersing flow are also analyzed, and the spall fracture mechanism is explored. Thus, the dominating forces determining the dispersing liquid flow are revealed, that is, the stretching and shearing action due to the interaction of two reflecting rarefaction waves in opposite propagating directions. The influence of container shell strength on the dispersing liquid flow is also investigated, and the characters of cavitation layered in liquid before shell rupturing are uncovered. Results revealed that different shell material results in different cavitating layers. Then the different cavitating layers drive the different dynamic liquid dispersing process coming into being. The metastable liquid states caused by pressure drop and cavi-tation generation are discussed.     

Robust TDOA/FDOA estimation from emitter signals for hybrid localization using UAVs

This paper considers the time difference of arrival (TDOA) and frequency difference of arrival (FDOA)estimation problem for joint localization using unmanned aerial vehicles (UAVs),involving range migration (RM) and Doppler ambiguity within observation interval.A robust estimation method based on interpolation and resampling is proposed.Specifically,the interpolation artificially increases the pulse repetition frequency (PRF).After that,the resampling eliminates the coupling between range frequency and slow time.Finally,a coherent integration step based on inverse discrete Fourier transform (IDFT) is used to achieve parameter estimation and suppress the grating lobes caused by interpolation.The proposed method could be efficiently implemented by fast Fourier transform (FFF),inverse FFT (IFFF) and non-uniform FFT (NUFFT) without parameter searching procedures.Numerical experiments indicate that the proposed method has nearly optimal anti-noise performance but much lower computational complexity than the maximum likelihood estimator,which makes it more competitive in practical applications.     

海洋环境影响声自导鱼雷的弹道分析与动态仿真

针对海洋环境引起的声自导鱼雷的声探测偏差问题,基于Argo资料,运用动态和对比分析,研究了鱼雷搜索和自导两个阶段中海洋环境对其声探测的影响机制、鱼雷声线轨迹偏差的纠正对策并进行仿真实现。结果表明:在搜索段,海况对鱼雷发现目标的时机具有显著的影响;在自导段,垂直温盐梯度的存在使鱼雷弹道产生偏差、遭遇时间变短、总航程缩短、最大需用过载变大,采取相应的纠正对策可以有效地降低鱼雷的脱靶量、提高自导性能。